EP1213221A1 - Joint d'étanchéité pour un propulseur à boítier extérieur - Google Patents
Joint d'étanchéité pour un propulseur à boítier extérieur Download PDFInfo
- Publication number
- EP1213221A1 EP1213221A1 EP01126239A EP01126239A EP1213221A1 EP 1213221 A1 EP1213221 A1 EP 1213221A1 EP 01126239 A EP01126239 A EP 01126239A EP 01126239 A EP01126239 A EP 01126239A EP 1213221 A1 EP1213221 A1 EP 1213221A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- air
- pressure
- pod
- compressed air
- chamber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H23/00—Transmitting power from propulsion power plant to propulsive elements
- B63H23/32—Other parts
- B63H23/321—Bearings or seals specially adapted for propeller shafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H2005/075—Arrangements on vessels of propulsion elements directly acting on water of propellers using non-azimuthing podded propulsor units, i.e. podded units without means for rotation about a vertical axis, e.g. rigidly connected to the hull
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
- B63H2005/1254—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
- B63H2005/1254—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis
- B63H2005/1258—Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis with electric power transmission to propellers, i.e. with integrated electric propeller motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H23/00—Transmitting power from propulsion power plant to propulsive elements
- B63H23/32—Other parts
- B63H23/321—Bearings or seals specially adapted for propeller shafts
- B63H2023/327—Sealings specially adapted for propeller shafts or stern tubes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
Definitions
- the present invention relates to a sealing device for pod propeller propulsion systems.
- a pod propeller propulsion system in which an electrical power generated by a diesel engine in the hull is transformed into an electric signal by an electric system, and the signal is transmitted to an electric motor in the pod rotatably mounted on the stern of the hull by means of a wire, so that the propeller is rotated by a propeller shaft connected to the motor (for example, "AZIPOD", a product of ABB Azipod) has been a focus of attention.
- AZIPOD a product of ABB Azipod
- this system Since the pod is freely rotatable outside the hull, this system has various advantages such that a steering apparatus is not necessary and the steerage is improved; that inboard noise and vibration can be reduced because it is electrically propelled; that the variation of design such as to dispose the engine on the bow-side of the hull expands; and the like.
- the sealing device employed in this case comprises a pod provided at the stern of the hull in such a manner that it is able to rotate freely about the vertical axis, a cylindrical casing connected to the pod on the stern-side of the hull, a propeller shaft coaxially inserted into the casing and connected to the electric motor disposed in the pod, and a plurality of seal ring to be brought into sliding contact with the outer periphery of the shaft to seal off outside water.
- an air-seal stern tube sealing device in which sliding load on the lip of the seal ring is lowered to improve durability of the seal ring by supplying compressed air to an air chamber defined between an adjacent pair of seal rings out of a plurality of seal rings to constantly blow off air from the chamber toward outboard water (See Japanese Examined Utility Model Publication No. 35249/1993, and Japanese Unexamined Patent Application Publication No. 304005/1999), or by supplying compressed air having air pressure which varies corresponding to variation in draft pressure and is lower than the draft pressure by a predetermined pressure difference into the air chamber (See Japanese Patent Publication No.2778899) is known.
- the seal ring may be damaged at an early stage and accordingly lubricant leaks outboard, which may result in environmental pollution. Therefore, it is believed that the durability of the seal ring is improved by adopting the above-described air-seal stern tube sealing device employed in the normal marine vessel propulsion system to the rear portion of the pod that constitutes the pod propeller propulsion system.
- the pod propeller propulsion system may be fatally damaged with mere adoption of the conventional air-seal stern tube sealing device to the rear portion of the pod.
- an object of the present invention to provide an air-seal type sealing device for pod propeller propulsion systems, wherein compressed air can be supplied to an air chamber provided on the rear-side of a pod while effectively preventing leakage of outside water into the pod, so that durability of the seal ring is increased without breakdown or corrosion of internal equipment in the pod.
- the present invention provides a sealing device for pod propeller propulsion system comprising first air supplying means for supplying compressed air into an air chamber defined between an adjacent pair of seal rings out of a plurality of seal rings, and second air supplying means for supplying compressed air having air pressure higher than that in the air chamber and varying corresponding to variations in draft pressure into a pod.
- the first air supplying means supplies compressed air into the air chamber in a casing connected to the rear-side of the pod, the sliding load on the lips of the seal rings for defining the air chamber is reduced, thereby improving durability of the seal ring.
- the second air supplying means supplies compressed air having air pressure higher than that in the air chamber and varying corresponding to variations in draft pressure into the pod, even when outside water enters into the air chamber because of the sliding load on the lips of the seal rings is reduced as described above, outside water is effectively prevented from being leaked into the pod.
- the sliding load acting upon the lips of the seal rings can be reduced by supplying compressed air to the air chamber provided on the rear-side of the pod by means of the first air supplying means while effectively preventing outside water from leaking into the pod by means of the second air supplying means, and thus the durability of the seal ring can be increased without breakdown or corrosion of the internal equipment of the pod.
- a lubricant chamber between the seal ring on the front-side out of a pair of seal rings for defining the air chamber and a next seal ring located further on the front-side and provide liquid supplying means for supplying a liquid lubricant into the lubricant chamber.
- a lubricant chamber defined between the seal ring and a seal ring located further on the rear-side is filled with lubricant highly viscous to the extent that it cannot be blown off outside the casing even by compressed air injected from the air chamber.
- lubricant in the lubricant chamber positioned on the rear-side of the air chamber has a high viscosity to the extent that it cannot be blown off outside the casing, even when the pressure of compressed air is increased to the extent that air is blown out from the air chamber, the lubricant is prevented from being scattered out of the casing and thus environmental pollution can be prevented in advance.
- lubricant filled in the lubricant chamber is highly viscous as described above, it is not necessary to add another seal ring on the rear-side for preventing oil leakage, whereby the axial dimension of the sealing device may be reduced.
- the first air supplying means comprising a first compressed air source, an air control unit for setting the pressure of compressed air from the compressed air source to the extent that air is blown off outside of the casing from the seal ring on the rear-side out of a pair of seal rings that define the air chamber, and an air piping for conducting the compressed air passed through the air control unit to the air chamber may be employed.
- a second air supplying means comprising a second compressed air source, an air relay for setting the air pressure of the compressed air from the second compressed air source to a predetermined output pressure with the air pressure in the air piping as a pilot pressure, and a pressurizing piping for applying the output pressure set at the air relay to the interior of the pod, and by setting the output pressure of the air relay slightly higher than the air pressure in the air chamber, compressed air having air pressure higher than that in the air chamber and varying corresponding to variations in draft pressure can be supplied into the pod.
- the first air supplying means comprising a first compressed air source, an air control unit for setting pressure of compressed air from the compressed air source to a predetermined pressure and flow rate, a detecting piping for blowing off the compressed air passed through the air control unit directly to outside water without passing through the seal ring to detect the draft pressure, a first air relay for setting pressure of compressed air from the first compressed air source to predetermined output pressure corresponding to the air pressure in the detecting piping as a pilot pressure, and an air piping for applying the output pressure predetermined at the first air relay into the air chamber may be employed.
- the air pressure of the air chamber can be set to the extent that air is blown off therefrom.
- the output pressure of the first air relay is set to almost the same value as the air pressure in the detecting piping or slightly lower than that value, compressed air is not blown off from the air chamber and, hence, outboard leakage of the liquid lubricant out of the casing in association with its blowoff may be prevented in advance, and advantageously, the amount of air consumption may be reduced as low as possible.
- compressed air having air pressure higher than that in the air chamber and varying corresponding to variations in draft pressure can be supplied into the pod by employing the second air supplying means comprising a second compressed air source, a second air relay for setting pressure of compressed air from the second compressed air source to a predetermined output pressure corresponding to the air pressure in the detecting piping as a pilot pressure, and a pressurized piping for applying the output pressure set at the second air relay into the pod, and by setting the output pressure of the second air relay slightly higher than the air pressure in the air chamber.
- Figs. 1 to 3 show a first embodiment of a sealing device 1 according to the present invention.
- the sealing device 1 of this embodiment is designed for a pod propeller propulsion system 2.
- the propulsion system 2 comprises a pod 4 provided at a stern of a hull 3 as an example of a structure floating on the water so as to rotate freely about a vertical axis, a cylindrical casing 5 connected to the rear-side of the pod 4, and a propeller shaft 7 inserted coaxially into the casing 5 and connected to an electric motor 6 disposed in the pod 4.
- the end of the shaft 7 on the front-side (right end in Fig. 1) is supported by a thrust bearing 8 disposed at the front portion of the pod 4 so as to rotate freely but not to move in the axial direction, and the end of the shaft 7 on the rear-side (left end in Fig. 1) is supported by a radial bearing 9 disposed at the rear end of the pod 4 so as to rotate freely.
- the end of the shaft 7 on the rear-side projects outside the pod 4, and a propeller 10 is fixed on the projected end.
- the sealing device 1 of this embodiment is an external sealing device disposed outside the pod 4 on the rear-side thereof, while between the radial bearing 9 and the motor 6 in the pod 4 an internal sealing device 11 is provided.
- the sealing device 1 described above comprises the pod 4 provided at the stern of the hull 3 so as to rotate freely about the vertical axis, the cylindrical casing 5 connected to the rear-side of the pod 4, the propeller shaft 7 inserted coaxially into the casing 5 and connected to the electric motor 6 disposed in the pod 4, and a plurality of seal rings 12-15 in sliding contact with the outer periphery of the shaft 7 for sealing outside water W.
- the propeller shaft 7 comprises a shaft body 16 connected directly to the motor 6, and a cylindrical liner 17 mounted on the axial portion of the shaft body 16 corresponding to the casing 5, wherein the lip of each seal ring 12-15 having a proximal end fixed on the inner peripheral surface of the casing 5 is in sliding contact with the outer peripheral surface of the liner 17.
- the shaft 7 may be constructed only of the shaft body 16, without providing the liner 17.
- seal rings 12-15 in total for defining an air chamber 20 within the casing 5 and lubricant chambers 21, 22 on the rear side and front side thereof.
- the first seal ring 12 disposed at the rearmost position (left side in Fig. 2) and the second seal ring 13 disposed next to the first ring on the front-side are oriented in such a manner that the tip edges of the lips face toward the rear-side.
- the third seal ring 14 that is disposed at the third rearmost position and the fourth seal ring 15 disposed next to the third seal ring 14 on the front-side are oriented in such a manner that the tip edges of the lips thereof face toward the front-side (right side in Fig. 2).
- the lips of the seal rings 12-15 are all wound with ring-shaped garter springs 23 respectively.
- the chamber defined between the second seal ring 13 and the third seal ring 14 is used as an air chamber 20 the inside of which is pressurized by compressed air, and a chamber defined between the second seal ring 13 which is the rear-side one of a pair of seal rings 13, 14 defining the air chamber 20 and the first seal ring 12 that is disposed further on the rear-side thereof is used as the first lubricant chamber 21 which is to be filled with a high viscosity lubricant 24.
- the first lubricant chamber 21 is filled with the lubricant 24 formed of grease or the like that is highly viscous to the extent that it cannot be blown off outside the casing even by compressed air blown off from the air chamber 20.
- a chamber defined between the third seal ring 14 which is the front-side one of a pair of seal rings 13, 14 defining the air chamber 20 and the fourth seal ring 14 disposed further on the front-side thereof is used as the second lubricant chamber 22 which is filled with a liquid lubricant 25 having sufficient fluidity by liquid supplying means 37 described later.
- the sealing device 1 of this embodiment comprises a first air supplying means 26 for supplying compressed air into the air chamber 20, and a second air supplying means 27 for supplying compressed air having air pressure higher than the air pressure P1 in the air chamber 20 and varying corresponding to variations in draft pressure P into the pod 4.
- the first air supplying means 26 comprises a first compressed air source 28 including a compressor and the like disposed in the hull 3, an air control unit 29 for setting pressure of compressed air from the first compressed air source 28 to the extent that air is blown off outside the casing from the second seal ring 13 on the rear-side out of a pair of seal rings 13, 14 defining the air chamber 20, and an air piping 30 introducing compressed air passed through the air control unit 29 to the air chamber 20.
- the air control unit 29 is provided with a pressure reducing valve 31 and a flow regulating valve 32 connected at a downstream side thereof.
- the first compressed air source 28 supplying compressed air of 7-8 (kg/cm 2 ) is used and then the air pressure is reduced by the pressure reducing valve 31 to about 2-3 (kg/cm 2 ).
- the flow rate of compressed air is set to approximately 10-40 (Nl/min.) by the flow regulating valve 32 to supply compressed air at a constant flow rate to the air chamber 20, so that compressed air is regularly blown off outside the casing from the lip of the second seal ring 13.
- the air pressure P1 in the air chamber 20 is set to P+0.1 (kg/cm 2 ) by the blowoff of compressed air described above, where the draft pressure at the center of the propeller shaft 7 of outside water W is P (kg/cm 2 ), and thus the air pressure P1 is controlled to vary corresponding to variations of the draft pressure P with regularly keeping a level higher than the draft pressure P by a constant pressure difference.
- the second air supplying means 27 comprises a second compressed air source 34 including a compressor and the like disposed in the hull 3, an air relay 35 for setting pressure of compressed air from the second compressed air source 34 to a predetermined output pressure with the air pressure in the air piping 30 as a pilot pressure, and a pressurizing piping 36 for applying the output pressure set at the air relay 35 to the interior of the pod 4.
- the sealing device 1 of this embodiment comprises the liquid supplying means 37 including an oil pump and the like for supplying the liquid lubricant 25 into the second lubricant chamber 22, and a drain circuit 38 connected to the air chamber 20 for collecting the liquid lubricant 25 leaked into the air chamber 20 during the supply thereof or outside water W within the pod 4 or the hull 3.
- the drain circuit 38 is constructed of a discharge pipeline 39 connected to the air chamber 20, and a drain tank 40 disposed in the hull 3 or the pod 4.
- the liquid supplying means 37 may be constructed to pump the liquid lubricant 25 little by little at a constant flow rate, or to pump the liquid lubricant 25 intermittently at constant intervals. Though the drain tank 40 and the liquid supplying means 37 may be disposed in the pod 4 if it has any room for them, it is preferable to dispose them in the hull 3 so that the pod 4 can be miniaturized.
- the first air supplying means 26 supplies compressed air into the air chamber 20 in the casing 5 that is connected to the rear side of the pod 4, the sliding load on the lips of the respective seal rings 13, 14 defining the air chamber 20 is reduced, thereby improving durability of the seal rings 13, 14.
- the lip of the ring 13 is hardly brought into sliding contact with the outer peripheral surface of the propeller shaft 7, thereby significantly increasing the lifetime of the second seal ring 13.
- the second air supplying means 27 is constructed to supply compressed air having air pressure higher than the air pressure P1 in the air chamber 20 and varying corresponding to variations in draft pressure P in the pod 4, even when outside water W enters into the air chamber 20 by reducing the sliding load on the lips of the seal rings 13, 14 as described above, further leakage of outside water W into the pod 4 is effectively prevented.
- the sliding load on the lips of the seal rings 13, 14 may be reduced by supplying compressed air into the air chamber 20 disposed on the rear side of the pod 4 by the first air supplying means 26 while effectively preventing leakage of outside water W into the pod 4 by means of the second air supplying means 27. Therefore, durability of the seal rings 13, 14 may be improved without inducing breakdown or corrosion of the internal equipment of the pod 4.
- the liquid supplying means 37 for supplying the liquid lubricant 25 into the second lubricant chamber 22 is provided and the drain circuit 38 is connected to the air chamber 20, even when the liquid lubricant 25 or outside water W leaks into the air chamber 20, they can be collected within the hull. Therefore, the seal ring 14 may be maintained in a lubricated state while preventing environmental pollution in association with the blowoff of the liquid lubricant 25 outside the casing.
- the lubricant 24 in the first lubricant chamber 21 is highly viscous to the extent that it cannot be blown off outside the casing, the lubricant 24 is prevented from being scattered outside the casing even when the pressure of compressed air is increased to the extent that air is blown off from the air chamber 20, and thus environmental pollution may be prevented in advance.
- the axial dimension of the sealing device 1 may be reduced since it is not necessary to provide an additional seal ring on the rear-side for preventing oil leakage.
- Fig. 3 shows a modification of the second lubricant chamber 22.
- the fourth seal ring 15 constituting the second lubricant chamber 22 is disposed in such a manner that the tip edge of the lip thereof faces toward the rear-side.
- the second lubricant chamber 22 is defined between a pair of seal rings 14 and 15 the tip edges of the lips of which face with each other, leakage of the liquid lubricant 25 into the pod 4 may be prevented more effectively.
- the relief pressure of the safety valve 41 should be set to a level approximately 0.2 (kg/cm 2 ) higher than the air pressure P2 in the pod 4.
- Fig. 4 is a second embodiment of the sealing device 1 according to the present invention.
- first embodiment is constructed to blow off compressed air through the seal ring
- second embodiment is constructed in such a manner that the air pressure in the air chamber can be varied by blowing off compressed air toward outside water without passing through the seal ring.
- Other structures are almost the same.
- the first air supplying means 26 of this embodiment comprises a first compressed air source 43 including a compressor and the like disposed in the hull 3, and an air control unit 44 for setting pressure of compressed air from the compressed air source 43 to a predetermined pressure and a flow rate, a detecting piping 45 for blowing off compressed air passed through the air control unit 44 directly toward outside water W without passing through the seal rings 12, 13 to detect the draft pressure P, a first air relay 46 for setting pressure of compressed air from the first compressed air source 43 to a predetermined output pressure with the air pressure in the detecting piping 45 as a pilot pressure, and an air piping 47 for applying the output pressure predetermined at the first air relay 46 into the air chamber 20.
- a first compressed air source 43 including a compressor and the like disposed in the hull 3, and an air control unit 44 for setting pressure of compressed air from the compressed air source 43 to a predetermined pressure and a flow rate, a detecting piping 45 for blowing off compressed air passed through the air control unit 44 directly toward outside water W without passing through the seal rings
- the air control unit 44 of this embodiment comprises a pressure reducing valve 48, a flow regulating valve 49 connected at the downstream side thereof, and the first air relay 46. While the discharge port of the detecting piping 45 is disposed at the proximal portion of the casing 5 in the figure, the discharge port may be disposed on the pod 4 or the hull 3.
- the air pressure of the air chamber 20 can be set to the extent that compressed air is blown off therefrom as in the case of the first embodiment.
- the output pressure of the first air relay 46 may be set to almost the same value as the air pressure in the detecting piping 45 or slightly lower than that value. In this case, since compressed air is not blown off from the air chamber 20, leakage of the liquid lubricant 25 out of the casing in association with its blowoff may be prevented in advance, and advantageously, the amount of air consumption may be reduced as low as possible.
- the second air supplying means 27 comprises a second compressed air source 50 including a compressor and the like disposed in the hull 3, a second air relay 51 for setting pressure of compressed air from the second compressed air source 50 to a predetermined output pressure with the air pressure in the detecting piping 45 as a pilot pressure, and a pressurized piping 52 for applying the output pressure set at the second air relay 51 into the pod 4.
- the second air supplying means 27 by setting the output pressure of the second air relay 52 to a value slightly higher than the air pressure P1 in the air chamber 20, compressed air having air pressure higher than the air pressure P1 in the air chamber 20 and varying corresponding to variations in the draft pressure P may be supplied into the pod 4.
- the present invention is not limited to the respective embodiments described above, and various modifications are possible.
- the construction in which the first seal ring 12 is omitted and thus the first lubricant chamber 21 is not provided is also applicable.
- pod propeller propulsion system 2 provided on the stern portion of the hull 3 as described above may be provided also on the bow portion or central portion of the full 3, or various structures floating on the water including an excavation plant of offshore oil fields, floating aerodromes, and the like.
- the present invention relates to a sealing device, which can be utilized to seal around the shaft of the pod propeller propulsion system provided at the rear portion of the hull so as to rotate freely about the vertical axis.
- a sealing device for pod propeller propulsion systems comprises: a pod (4) provided on a structure (3) floating on the water so as to rotate freely about a vertical axis; a cylindrical casing (5) connected to the rear-side of the pod (4); a propeller shaft (7) inserted coaxially into the casing (5) and connected to an electric motor (6) disposed in the pod (4); a plurality of seal rings (12, 13, 14, 15) in sliding contact with the outer periphery of the shaft (7) for sealing outside water (W); first air supplying means (26) for supplying compressed air into an air chamber (20) defined between a pair of adjacent seal rings (13, 14) out of the plurality of seal rings (12, 13, 14, 15); and second air supplying means (27) for supplying compressed air having air pressure higher than air pressure (P1) in the air chamber (20) and varying corresponding to variations in draft pressure (P) into the pod (4).
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Sealing Devices (AREA)
- Sealing With Elastic Sealing Lips (AREA)
- Sealing Of Bearings (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000374745 | 2000-12-08 | ||
JP2000374745 | 2000-12-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1213221A1 true EP1213221A1 (fr) | 2002-06-12 |
EP1213221B1 EP1213221B1 (fr) | 2004-02-18 |
Family
ID=18843877
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01126239A Expired - Lifetime EP1213221B1 (fr) | 2000-12-08 | 2001-11-05 | Joint d'étanchéité pour un propulseur à boítier extérieur |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1213221B1 (fr) |
DE (1) | DE60102064T2 (fr) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005090797A1 (fr) * | 2004-03-17 | 2005-09-29 | Imi Norgren Limited | Vanne de regulation de debit |
NL1025959C2 (nl) * | 2004-04-15 | 2005-10-18 | Ihc Holland Nv | Afdichtingsconstructie. |
US7189126B2 (en) * | 2001-06-14 | 2007-03-13 | Abb Oy | Ship's propulsion arrangement and method |
WO2010100094A3 (fr) * | 2009-03-02 | 2011-05-12 | Siemens Aktiengesellschaft | Turbomachine comportant un carter à étanchéité améliorée |
FR2955557A1 (fr) * | 2010-01-22 | 2011-07-29 | Vanessa Batlle | Dispositif destine a assurer l'etancheite sur l'arbre de l'helice d'un bateau de toutes dimensions equipe d'un ou plusieurs moteurs |
WO2016071565A1 (fr) * | 2014-11-03 | 2016-05-12 | Abb Oy | Agencement d'étanchéité pour navire, unité de propulsion, navire et procédé d'étanchéité pour arbre porte-hélice de navire |
CN110203363A (zh) * | 2019-06-10 | 2019-09-06 | 山东华宇工学院 | 一种提高潜水艇深海航速的装置 |
EP3656655A1 (fr) * | 2018-11-23 | 2020-05-27 | Caterpillar Propulsion Production AB | Système de détection de fuites pour propulseur d'azimut |
EP4043335A1 (fr) * | 2021-02-16 | 2022-08-17 | ABB Schweiz AG | Procédé et agencement d'étanchéité d'un arbre d'hélice situé sous l'eau |
RU2778797C1 (ru) * | 2021-02-16 | 2022-08-25 | Абб Швайц Аг | Способ и компоновка для уплотнения вала винта, расположенного под водой |
EP4197898A1 (fr) * | 2021-12-14 | 2023-06-21 | ABB Oy | Agencement de drainage d'une unité de propulsion |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009052433A1 (de) * | 2009-11-10 | 2011-05-12 | Schottel Gmbh | Schiffsantrieb |
DE102013209682B4 (de) * | 2013-05-24 | 2017-12-28 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Gehäuse für ein propellerantriebsaggregat |
Citations (4)
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DE3815655A1 (de) * | 1988-05-07 | 1989-11-16 | Blohm Voss Ag | Abdichtung fuer rotierende wellen, insbesondere stevenrohrabdichtung |
US5209497A (en) * | 1990-09-05 | 1993-05-11 | Blohm+Voss Ag | Sealing apparatus for rotating shafts, in particular stern tube seal for the propeller shafts of a ship |
EP0590867A1 (fr) * | 1992-09-28 | 1994-04-06 | Kvaerner Masa-Yards Oy | Installation de propulsion marine |
US5683278A (en) * | 1994-09-24 | 1997-11-04 | Blohm Voss Holding Ag | Stern tube seal with a pressure control system to adjust to the changing draft of ocean-going ships |
-
2001
- 2001-11-05 DE DE60102064T patent/DE60102064T2/de not_active Expired - Lifetime
- 2001-11-05 EP EP01126239A patent/EP1213221B1/fr not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3815655A1 (de) * | 1988-05-07 | 1989-11-16 | Blohm Voss Ag | Abdichtung fuer rotierende wellen, insbesondere stevenrohrabdichtung |
US5209497A (en) * | 1990-09-05 | 1993-05-11 | Blohm+Voss Ag | Sealing apparatus for rotating shafts, in particular stern tube seal for the propeller shafts of a ship |
EP0590867A1 (fr) * | 1992-09-28 | 1994-04-06 | Kvaerner Masa-Yards Oy | Installation de propulsion marine |
US5683278A (en) * | 1994-09-24 | 1997-11-04 | Blohm Voss Holding Ag | Stern tube seal with a pressure control system to adjust to the changing draft of ocean-going ships |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7189126B2 (en) * | 2001-06-14 | 2007-03-13 | Abb Oy | Ship's propulsion arrangement and method |
WO2005090797A1 (fr) * | 2004-03-17 | 2005-09-29 | Imi Norgren Limited | Vanne de regulation de debit |
NL1025959C2 (nl) * | 2004-04-15 | 2005-10-18 | Ihc Holland Nv | Afdichtingsconstructie. |
EP1586798A1 (fr) * | 2004-04-15 | 2005-10-19 | IHC Holland NV | Dispositif de joint d'étanchéité |
WO2010100094A3 (fr) * | 2009-03-02 | 2011-05-12 | Siemens Aktiengesellschaft | Turbomachine comportant un carter à étanchéité améliorée |
FR2955557A1 (fr) * | 2010-01-22 | 2011-07-29 | Vanessa Batlle | Dispositif destine a assurer l'etancheite sur l'arbre de l'helice d'un bateau de toutes dimensions equipe d'un ou plusieurs moteurs |
KR101899337B1 (ko) | 2014-11-03 | 2018-09-17 | 에이비비 오와이 | 선박을 위한 밀봉 장치, 추진 장치, 선박, 및 선박의 프로펠러 샤프트를 밀봉하기 위한 방법 |
KR20170069278A (ko) * | 2014-11-03 | 2017-06-20 | 에이비비 오와이 | 선박을 위한 밀봉 장치, 추진 장치, 선박, 및 선박의 프로펠러 샤프트를 밀봉하기 위한 방법 |
WO2016071565A1 (fr) * | 2014-11-03 | 2016-05-12 | Abb Oy | Agencement d'étanchéité pour navire, unité de propulsion, navire et procédé d'étanchéité pour arbre porte-hélice de navire |
RU2670552C1 (ru) * | 2014-11-03 | 2018-10-23 | Абб Ой | Уплотнительное устройство для судна, силовая установка, судно и способ уплотнения гребного вала судна |
EP3656655A1 (fr) * | 2018-11-23 | 2020-05-27 | Caterpillar Propulsion Production AB | Système de détection de fuites pour propulseur d'azimut |
WO2020104070A1 (fr) * | 2018-11-23 | 2020-05-28 | Caterpillar Propulsion Production Ab | Système de détection de fuite pour propulseur d'azimut |
CN110203363A (zh) * | 2019-06-10 | 2019-09-06 | 山东华宇工学院 | 一种提高潜水艇深海航速的装置 |
EP4043335A1 (fr) * | 2021-02-16 | 2022-08-17 | ABB Schweiz AG | Procédé et agencement d'étanchéité d'un arbre d'hélice situé sous l'eau |
RU2778797C1 (ru) * | 2021-02-16 | 2022-08-25 | Абб Швайц Аг | Способ и компоновка для уплотнения вала винта, расположенного под водой |
CN114940255A (zh) * | 2021-02-16 | 2022-08-26 | Abb瑞士股份有限公司 | 用于密封位于水下的螺旋桨轴的方法和装置 |
US11702182B2 (en) | 2021-02-16 | 2023-07-18 | Abb Schweiz Ag | Method and arrangement for sealing a propeller shaft located under water |
CN114940255B (zh) * | 2021-02-16 | 2024-05-14 | Abb瑞士股份有限公司 | 用于密封位于水下的螺旋桨轴的方法和装置 |
EP4197898A1 (fr) * | 2021-12-14 | 2023-06-21 | ABB Oy | Agencement de drainage d'une unité de propulsion |
Also Published As
Publication number | Publication date |
---|---|
DE60102064T2 (de) | 2004-12-30 |
DE60102064D1 (de) | 2004-03-25 |
EP1213221B1 (fr) | 2004-02-18 |
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